Computational Analysis Of Incompressible Viscous Flow Over Single And Multi-Element Airfoils
The flow-field around a multi-element airfoil with leading-edge slat and trailing-edge flap in landing configuration was performed as well as the prediction of the time dependent flow over a NACA 0012 airfoil. The two dimensional incompressible Navier-Stokes equations with a numerical method bas...
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| 格式: | Thesis |
| 语言: | 英语 英语 |
| 出版: |
2003
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| 在线阅读: | http://psasir.upm.edu.my/id/eprint/12152/1/FK_2003_11.pdf |